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Analysis and optimum design of rider-bicycle mechanisms: Design of bicycle parameters for a specified rider

✍ Scribed by XinJun Liu; Jing Wang; WeiYang Yu; JinHua Wu

Publisher
SP Science China Press
Year
2011
Tongue
English
Weight
760 KB
Volume
54
Category
Article
ISSN
1006-9321

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OPTIMUM DESIGN OF A HELICOPTER ROTOR FOR
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An aeroelastic analysis based on finite elements in space and time is used to model the helicopter rotor in forward flight. The rotor blade is represented as an elastic cantilever beam undergoing flap and lag bending, elastic torsion and axial deformations. The objective of the improved design is to